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C69300 Brass vs. CC140C Copper

Both C69300 brass and CC140C copper are copper alloys. They have 75% of their average alloy composition in common. There are 28 material properties with values for both materials. Properties with values for just one material (3, in this case) are not shown.

For each property being compared, the top bar is C69300 brass and the bottom bar is CC140C copper.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 110
120
Elongation at Break, % 8.5 to 15
11
Poisson's Ratio 0.32
0.34
Shear Modulus, GPa 41
44
Tensile Strength: Ultimate (UTS), MPa 550 to 630
340
Tensile Strength: Yield (Proof), MPa 300 to 390
230

Thermal Properties

Latent Heat of Fusion, J/g 240
210
Maximum Temperature: Mechanical, °C 160
200
Melting Completion (Liquidus), °C 880
1100
Melting Onset (Solidus), °C 860
1040
Specific Heat Capacity, J/kg-K 400
390
Thermal Conductivity, W/m-K 38
310
Thermal Expansion, µm/m-K 19
17

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 8.0
77
Electrical Conductivity: Equal Weight (Specific), % IACS 8.8
78

Otherwise Unclassified Properties

Base Metal Price, % relative 26
31
Density, g/cm3 8.2
8.9
Embodied Carbon, kg CO2/kg material 2.7
2.6
Embodied Energy, MJ/kg 45
41
Embodied Water, L/kg 310
310

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 47 to 70
34
Resilience: Unit (Modulus of Resilience), kJ/m3 400 to 700
220
Stiffness to Weight: Axial, points 7.4
7.3
Stiffness to Weight: Bending, points 19
18
Strength to Weight: Axial, points 19 to 21
10
Strength to Weight: Bending, points 18 to 20
12
Thermal Diffusivity, mm2/s 12
89
Thermal Shock Resistance, points 19 to 22
12

Alloy Composition


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Chromium (Cr), % 0
0.4 to 1.2
Copper (Cu), % 73 to 77
98.8 to 99.6
Iron (Fe), % 0 to 0.1
0
Lead (Pb), % 0 to 0.090
0
Manganese (Mn), % 0 to 0.1
0
Nickel (Ni), % 0 to 0.1
0
Phosphorus (P), % 0.040 to 0.15
0
Silicon (Si), % 2.7 to 3.4
0
Tin (Sn), % 0 to 0.2
0
Zinc (Zn), % 18.4 to 24.3
0
Residuals, % 0 to 0.5
0